• 제목/요약/키워드: stage combustion

검색결과 321건 처리시간 0.03초

점화시스템의 종류와 가솔린 엔진 성능과의 상관관계에 대한 연구 (I) (A Study on Relationship between Ignition Systems and the Performances of Gasoline Engines (I))

  • 선우명호;송정훈
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1998년도 추계학술대회 논문집 학회본부 C
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    • pp.966-969
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    • 1998
  • Fast burning achieves higher efficiency, and reduces cycle variations which is able to improve vehicle driveability. Furthermore, the greater resistance to knock with fast burning can allow the fuel economy advantages associated with higher compression ratio to be realized. One way of increasing the combustion speed is to enhance the performance of ignition systems which were able to reduce the early period of combustion. It is well known that shortening the initial stage of combustion also reduces the cyclic variations. This literature survey deals with the papers which have studied the ignition process or various ignition systems. Those systems increasing the combustion speed, extending the lean misfire limit, reducing the exhaust gas and stabilizing the operating condition of the spark ignition engine by modifying the ignition process or increasing ignition energy.

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열분해 소각시설에서의 일반폐기물의 연소특성 (Combustion Characteristics of Municipal Wastes in Pyrolysis Incinerator)

  • 박명호
    • 한국기계기술학회지
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    • 제13권4호
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    • pp.149-156
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    • 2011
  • In case of domestic pyrolysis dry distillation gassification technology, it stays at the stage of its early introduction and development. Moreover, the companies possessed of this technology are limited to Japan and some countries in Europe, and domestic operative performance of this system is nominal, so there exist a lot of difficulties in securing its basic data. In addition, considering its operation and management, there happens a corrosion of metals by the production of corrosive gases in time of combustion of waste, and there arise a problem of occurrence of low temperature corrosion on exterior casing or gas ducts of a combustion chamber due to the high temperature corrosion around the burner of an incinerator, lowering the durability of an incinerator. Therefore, this study looked at the problems arising in time of incineration by understanding the characteristics of the pyrolysis dry distillation gassification incinerating facility, and did research on the improvement plan for durability of an incinerator for more economic, efficient waste incineration.

연소기 연소시험설비 고주파 계측 시스템 설계 (Design of High-Frequency Data Acquisition System for Combustor Combustion Test Facility)

  • 안규복;강동혁;최환석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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    • pp.461-464
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    • 2012
  • 한국형발사체 3단에 사용될 7톤급 액체로켓엔진 연소기의 연소시험을 위해 기존 지상연소시험장 고주파 계측 시스템을 개량하였다. 본 논문에서는 개량된 고주파 계측 시스템의 설계 및 주요 기능을 설명하였다.

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레이저 유도 공동 점화방식을 이용한 예혼합기 연소 특성 향상 (Combustion Enhancemen of Premixed Mixtures Using Laser-Induced Cavity Ignition)

  • 모하메드하산;고영성;정석호
    • 한국자동차공학회논문집
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    • 제7권6호
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    • pp.8-16
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    • 1999
  • In this study, a new type of laser-induced ignition using a conical cavity has been developed to utilize all the available incident laser energy. In the method, it is possibile to ignite combustible methane/air mixtures by directing a laser beam of a constant small diameter into a small conical cavity, without focusing the laser beam. Shadow graphs for the early stage of combustion process show that a hot gas jet is ejected from the cavity, especially with lean mixture. After a very show time, the hot gas jet finishes issuing and the flame behavior is quite similar to flame propagation initiated by a conventional spark ignition. The combustion process using the new method exhibits more rapid pressure increase and a higher maximum pressure rise than that of the center ignition using laser-induced spark, with significant decrease in the combustion time. Also, the new ignition method is numerically modeled to simulate the flame kernel development and subsequent combustion process using the KIVA-IIcode. The calculated results show satisfactory agreement with experimental results.

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함산소계 및 파라핀계 혼합 경유 및 저질유 액적의 연소특성에 관한 연구 (Study on Combustion Characteristics of Diesel Fuel and Low Quality Oil Droplet with Additive Oxygenate and Paraffin)

  • 김봉석;소천영지
    • Journal of Advanced Marine Engineering and Technology
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    • 제30권5호
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    • pp.552-561
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    • 2006
  • The single droplet combustion characteristics of diesel fuel and low quality oil with additive oxygenate and paraffin under high ambient temperature and atmospheric pressure were investigated in the study. The results of the study may are concluded as follows: In the combustion of diesel fuel and low quality oil droplet with additive of oxygenate and paraffin. the dimensionless droplet size of $(D/Do)^2$ was linearly decreased with time. A fuel droplet with low boiling temperature additives and in high boiling temperature base fuel evaporates and burns faster than usual base fuel. Especially. these trends were remarkably obtained by decreasing boiling point and increasing blending contents of additives in case of oxygenated agents rather than n-paraffin agents. This rapid burning may result from so-called 'micro-explosion' and its burning intensity varies with the types of additives. The results above may suggest that rapid evaporation of oxygenate additive in the middle stage of combustion can contribute much to combustion improvement of blended fuels.

PROPAGATION PROCESSES OF NEWLY DEVELOPED PLASMA JET IGNITER

  • Ogawa, Masaya;Sasaki, Hisatoshi;Yosgida, Koji;Shoji, Hideo;Tanaka, Hidenori
    • International Journal of Automotive Technology
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    • 제3권1호
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    • pp.9-16
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    • 2002
  • In plasma jet ignition, combustion enhancement effects occur toward the plasma jet issuing direction. Therefore, when the igniter is attached at the center of a cylindrically shaped combustion chamber, plasma jet should issue toward the round combustion chamber wall. The plasma jet igniter that had an annular circular orifice has been developed. The purpose of this study is to elucidate the relationship between the newly developed plasma Jet igniter configuration and combustion enhancement effects. In this newly developed plasma Jet igniter, flame front wrinkle appears on the flame front and flame propagates rapidly. Plasma Jet influences on the flame propagation far long period when the plasma jet igniter has issuing angle 90 degrees and large cavity volume, because the plasma jet only lasts several ms. However, in the early stage of combustion, flame front area of issuing angle 45 degrees is larger than that of 90 degrees, because the initial flame kernel is formed by the plasma jet.

Multi-cavity Piston에 의한 바이오디젤유의 연소성 향상에 관한 연구 (The Study for Improving the Combustion of Biodiesel Fuel using Multi-cavity Piston)

  • 방중철;김용재;박철환
    • 한국연소학회지
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    • 제20권4호
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    • pp.26-33
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    • 2015
  • American NREL (National Renewable Energy Laboratory) reported that BD20 could reduce PM, CO, SOx and cancerogenic matters by 13.6%, 9.3%, 17.6% and 13% respectively, compared to diesel fuel. BD20 has been being tested on garbage trucks and official vehicles at Seoul City, which is positive on air environment, but negative on combustion by higher viscosity in winter season. This study investigated the combustion characteristics by employing multi cavity piston for improving the deterioration of combustibility caused by the higher viscosity of the biodiesel fuel such as BD20 with the combustion flames taken by a high speed camera and the cylinder pressure diagram. A 4-cycle single cylinder diesel engine was remodeled to a visible 2-cycle engine for taking the flame photographs, which has a common-rail injection system. The test was done at laboratory temperature of about $4{\sim}5^{\circ}C$.

가스발생기 사이클 엔진 연소시험 중 재생냉각형 연소기의 내피 손상진단 (A Fault Diagnosis of Damage on Inner Liner of Regeneratively-Cooled Combustion Chamber during Gas Generator Cycle Engine Hot Firing Test)

  • 황도근;김현준;김종규;김문기;임병직;강동혁;주성민;최환석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.1165-1168
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    • 2017
  • 본 논문에서는 재생냉각형 연소기를 채용한 가스발생기 사이클 로켓엔진의 연소시험 중 연소기의 내피 손상을 진단하는 방안을 제시하였다. 이는 연소기 내피 손상 발생 시 연료가 유실되면서 두가지 방식의 연소기 연료유입량 예측값 차이에 변화가 발생하는 것에 착안한 방법으로 로켓엔진 시험 중 연소기 내피손상을 조기에 파악하여 추가 손상 방지에 기여할 수 있을 것으로 기대된다.

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直接噴射式 디이젤機關의 燃燒室形狀과 火焰의 發達 (The effect of air and spray turbulence in a D.I. diesel engine on the flame progress)

  • 방중철;태전간랑
    • 대한기계학회논문집
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    • 제11권1호
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    • pp.44-52
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    • 1987
  • 본 논문에서는 앞서의 연구들에서 얻은 연구성과를 실제의 디이젤기관에 적용 시켜 화염의 발달상태와 기관속도의 상승 등을 고찰하여, 그 유효성을 평가했다. 또 고온공기류덕트에서는 실험하기가 곤란했던, 분무자체에 족회운동을 일으킨 경우의 연 소과정에 대해서도 피스톤요부의 벽면에 충돌하는 분무의 각도를 변화시켜, 고속도 화 염사진으로 부터 검토했다.

H2O2-케로신 로켓을 초기 가속장치로 갖는 새로운 램젯 추진기관 (Novel Ramjet Propulsion System with H2O2-Kerosene Rocket as an Initial Accelerator)

  • 박근홍;임하영;권세진
    • 한국항공우주학회지
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    • 제36권5호
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    • pp.491-496
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    • 2008
  • 본 연구에서는 RBCC (Rocket Based Combined Cycle)엔진이나 기존 램제트 추진기관의 초기 추력 제공에 과산화수소 가스발생기를 이용하는 새로운 추진시스템을 제안하였고, 기초 연구 수행으로서 촉매 분해된 과산화수소 제트에 케로신을 분사하여 자연발화 및 연소 특성을 연구하였다. 과산화수소는 촉매 베드를 통하여 분해된 후 축소노즐을 통해 연소실로 분사됐으며 이 제트에 인젝터를 통하여 수직으로 케로신을 액상으로 분무하였다. 연소실내에서의 온도와 압력을 측정하여 점화를 확인하고 자연발화 특성을 조사하였다. 400°C의 연소실 온도와 연료와 산화제 혼합비 0.6이상에서 자연발화와 안정적인 연소가 가능하였다. 이 결과를 통하여 램제트의 새로운 초기 가속장치의 가능성을 확인할 수 있었다.